ILYUSHIN IL-14 Civil Aircraft Model Details

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General Information of ILYUSHIN IL-14

Developed From : Ilyushin Il-12

First Flight : 1 October 1950

Introduction : 1954 (Aeroflot)

Manufacturer : Ilyushin

National Origin : Soviet Union

Number Built : 1348

Primary Users : Soviet Air Force ;Aeroflot; Egyptian Air Force

Retired : 1998 (Vietnamese Air Force); 1998 (Syrian Air Force); 2005 (Russian CAA)

Role : Airliner

Status : Very few operational

General characteristics of ILYUSHIN IL-14

Capacity : 24-32 passengers

Crew : Four (flight crew)

Empty Weight : 12,600 kg (27,778 lb)

Height : 7.90 m (25 ft 11 in)

Length : 22.30 m (73 ft 2 in)

Max Takeoff Weight : 18,000 kg (39,683 lb)

Powerplant : 2 × Shvetsov ASh-82T 14 cylinder air-cooled radial engines, 1,417 kW (1,900 hp) each

Wing Area : 99.7 m² (1,073 ft²)

Wingspan : 31.70 m (104 ft 0 in)

Performance of ILYUSHIN IL-14

Maximum Speed : 417 km/h (225 kn, 259 mph)

Range : 1,305 km (705 nmi, 811 mi) (full payload)

Rate Of Climb : 5 m/s (900 fpm)

Service Ceiling : 7,400 m (24,280 ft)

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